Starck AS.20

AS.20
General information
Type	Experimental aircraft
National origin	France
Designer	André Starck
Number built	1
History
First flight	23 October 1942

Starck AS-20 3-view

The Starck AS.20 was an experimental single seat narrow-gap biplane built in France in the early 1940s. ^[1] Despite the occupation of France, construction continued into 1941.

Specifications

Data from ^[2]

General characteristics

• Crew: 1
• Length: 5.30 m (17 ft 5 in)
• Wingspan: 5.84 m (19 ft 2 in)
• Wing area: 8.00 m² (86.1 sq ft)
• Empty weight: 226 kg (498 lb)
• Gross weight: 373 kg (822 lb)
• Powerplant: 1 × Régnier 4D2 air-cooled flat four, 55 kW (74 hp)
• Propellers: 2-bladed

Performance

• Maximum speed: 240 km/h (150 mph, 130 kn)
• Range: 1,400 km (870 mi, 760 nmi)
• Service ceiling: 7,500 m (24,600 ft)

References

1. "Stark AS20 of 1942 - Rare Birds (6)". Falkeeinsgreatplanes.blogspot.com. 24 January 2010. Retrieved 10 March 2019.
2. "Starck AS-20". Aviafrance.com. Retrieved 10 March 2019.

External links

• "Matériel Volant: Avion Starck (Type A.S. 20 Moteur Régnier 74 CV.)". L'Aérophile (in French). Vol. 51, no. 4. April 1943. pp. 66–67.